OBTAINING THE CHANDRAYAAN-3 LANDER COORDINATES ON THE LUNAR SURFACE BY THE DOPPLER MEASUREMENTS OF THE TRANSMITTED SIGNAL WITH AN EARTH-BASED RECEIVING SYSTEM
Section: ASTRONOMICAL INSTRUMENTS AND METHODS
Authors:
1.
Institute of Applied Astronomy, Russian Academy of Sciences
2.
Institute of Applied Astronomy, Russian Academy of Sciences
3.
Institute of Applied Astronomy of the Russian Academy of Sciences
4.
Institute of Applied Astronomy, Russian Academy of Sciences
Type:
Сonference article
Published:
27.12.2024
Subject area:
UDC 52
UDC 53
UDC 520
UDC 521
UDC 523
UDC 524
UDC 52-1
UDC 52-6
CSCSTI 41.00
CSCSTI 29.35
CSCSTI 29.31
CSCSTI 29.33
CSCSTI 29.27
CSCSTI 29.05
Russian Classification of Professions by Education 03.06.01
Russian Classification of Professions by Education 03.05.01
Russian Classification of Professions by Education 03.04.03
Russian Library and Bibliographic Classification 2
Russian Library and Bibliographic Classification 223
Russian Trade and Bibliographic Classification 614
Russian Trade and Bibliographic Classification 6135
BISAC SCI004000 Astronomy
BISAC SCI005000 Physics / Astrophysics
UDC 53
UDC 520
UDC 521
UDC 523
UDC 524
UDC 52-1
UDC 52-6
CSCSTI 41.00
CSCSTI 29.35
CSCSTI 29.31
CSCSTI 29.33
CSCSTI 29.27
CSCSTI 29.05
Russian Classification of Professions by Education 03.06.01
Russian Classification of Professions by Education 03.05.01
Russian Classification of Professions by Education 03.04.03
Russian Library and Bibliographic Classification 2
Russian Library and Bibliographic Classification 223
Russian Trade and Bibliographic Classification 614
Russian Trade and Bibliographic Classification 6135
BISAC SCI004000 Astronomy
BISAC SCI005000 Physics / Astrophysics
Language:
English
Keywords:
ephemerides; Moon; space vehicles; techniques: radial velocities; telescopes
Abstract (English):
We determine the selenographic coordinates of the Chandrayaan-3 lander by Doppler measurements of its signal. The Chandrayaan-3 successfully landed in the south polar region of the Moon near the craters Manzinus and Simpelius on 23 August 2023 and had been transmitting scientific information and telemetry to Earth in the S and X-bands during 14 days. The accuracy of the obtained Doppler measurements do not allow unambiguous determination of the lander location on the lunar surface because the transmitter was degrading during the entire observing interval. For this reason, in our work we have evaluated the influence of the Doppler measurement characteristics on the accuracy of the transmitter location determination. It has been shown that for a signal with a relative frequency instability of the order of $10^{-13}$, the achievable accuracy of coordinate determination is about 34 meters.
We determine the selenographic coordinates of the Chandrayaan-3 lander by Doppler measurements of its signal. The Chandrayaan-3 successfully landed in the south polar region of the Moon near the craters Manzinus and Simpelius on 23 August 2023 and had been transmitting scientific information and telemetry to Earth in the S and X-bands during 14 days. The accuracy of the obtained Doppler measurements do not allow unambiguous determination of the lander location on the lunar surface because the transmitter was degrading during the entire observing interval. For this reason, in our work we have evaluated the influence of the Doppler measurement characteristics on the accuracy of the transmitter location determination. It has been shown that for a signal with a relative frequency instability of the order of $10^{-13}$, the achievable accuracy of coordinate determination is about 34 meters.
Keywords:
ephemerides; Moon; space vehicles; techniques: radial velocities; telescopes
ephemerides; Moon; space vehicles; techniques: radial velocities; telescopes
1. Brumberg V.A., Glebova N.I., Lukashova M.V., et al., 2004, Transactions of IAA RAS, 10
2. Duev D.A., Molera Calves G., Pogrebenko S.V., et al., 2012, Astronomy & Astrophysics, 541, id. A43
3. Marshalov D., Ping J., Li W., et al., 2020, Latvian Journal of Physics and Technical Sciences, 57, p. 22
4. Murphy T.W. Jr., Adelberger E.G., Battat J.B.R., et al., 2011, Icarus, 211, p. 1103
5. Park R.S., Folkner W.M., Williams J.G., et al., 2021, The Astronomical Journal, 161, id. 105
6. Shuygina N., Ivanov D., Ipatov A., et al., 2019, Geodesy and Geodynamics, 10, 2, p.150
7. Vasilyev M.V., Yagudina E.I., Krasinsky G.A., et al., 2022, Transactions of IAA RAS, 63, p. 28
